GB2197911B - Turbine shaft fuel pump - Google Patents

Turbine shaft fuel pump

Info

Publication number
GB2197911B
GB2197911B GB8715321A GB8715321A GB2197911B GB 2197911 B GB2197911 B GB 2197911B GB 8715321 A GB8715321 A GB 8715321A GB 8715321 A GB8715321 A GB 8715321A GB 2197911 B GB2197911 B GB 2197911B
Authority
GB
United Kingdom
Prior art keywords
fuel pump
turbine shaft
shaft fuel
turbine
pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
GB8715321A
Other versions
GB8715321D0 (en
GB2197911A (en
Inventor
Raymond Smith
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Teledyne Inc
Original Assignee
Teledyne Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to US06/890,869 priority Critical patent/US5042256A/en
Application filed by Teledyne Inc filed Critical Teledyne Inc
Publication of GB8715321D0 publication Critical patent/GB8715321D0/en
Publication of GB2197911A publication Critical patent/GB2197911A/en
Application granted granted Critical
Publication of GB2197911B publication Critical patent/GB2197911B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/236Fuel delivery systems comprising two or more pumps
    • Y02T50/671
GB8715321A 1986-07-28 1987-06-30 Turbine shaft fuel pump Expired - Fee Related GB2197911B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US06/890,869 US5042256A (en) 1986-07-28 1986-07-28 Turbine shaft fuel pump

Publications (3)

Publication Number Publication Date
GB8715321D0 GB8715321D0 (en) 1987-08-05
GB2197911A GB2197911A (en) 1988-06-02
GB2197911B true GB2197911B (en) 1991-03-20

Family

ID=25397253

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8715321A Expired - Fee Related GB2197911B (en) 1986-07-28 1987-06-30 Turbine shaft fuel pump

Country Status (5)

Country Link
US (1) US5042256A (en)
DE (1) DE3722530C2 (en)
FR (1) FR2602003B1 (en)
GB (1) GB2197911B (en)
IL (1) IL83050A (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5526640A (en) * 1994-05-16 1996-06-18 Technical Directions, Inc. Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall
DE69621906T2 (en) * 1996-03-13 2002-10-10 Tech Directions Inc Gas turbine
US6209309B1 (en) 1997-12-19 2001-04-03 Hamilton Sundstrand Corporation Pulse width modulated fuel flow control for an engine
DE19846976A1 (en) * 1998-10-12 2000-04-13 Bmw Rolls Royce Gmbh Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft
GB9902502D0 (en) * 1999-02-04 1999-03-24 Ripmax Plc Turbine engine
DE102004031783B4 (en) * 2004-07-01 2006-07-27 Markus Schmidt Gas turbine for aircraft engine has fuel supply system which exhibits wave-channel in which turbine shaft is swivel mounted and part of fuel supply takes place through shaft alley, which exhibits fuel outlets at its outer circumference
US7937946B1 (en) 2005-12-21 2011-05-10 Florida Turbine Technologies, Inc. Small gas turbine engine with lubricated bearings
US20090123310A1 (en) * 2007-11-12 2009-05-14 Chang Up Kim External inline LPG fuel pump
CN104534513B (en) * 2014-11-27 2017-09-15 北京华清燃气轮机与煤气化联合循环工程技术有限公司 Gas-turbine combustion chamber revolves jet mixing nozzle
CN106351747B (en) * 2016-11-21 2018-03-09 中国航空动力机械研究所 A kind of fuel oil supply system and method for small-power gas-turbine unit

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB699865A (en) * 1950-11-06 1953-11-18 W H Allen Sons & Company Ltd Improvements in or relating to gas turbines
GB719469A (en) * 1951-09-11 1954-12-01 Rolls Royce Improvements in or relating to fuel systems for internal combustion engines
GB727796A (en) * 1951-05-10 1955-04-06 Nat Res Dev Improvements relating to combustion equipment for burning liquid fuel and to gas turbine plant in which it is incorporated
GB837738A (en) * 1957-01-08 1960-06-15 Szydlowski Joseph Improvements in or relating to rotary injection devices for gas turbine combustion chambers
GB896223A (en) * 1959-05-22 1962-05-09 Bmw Triebwerkbau Gmbh Fuel induction through the rotor shaft of a gas turbine
GB917704A (en) * 1958-07-31 1963-02-06 Power Jets Res & Dev Ltd Combustion apparatus
GB955150A (en) * 1960-04-23 1964-04-15 Gasturbinenbau Und Energiemasc Improvements in or relating to gas turbines
GB1056338A (en) * 1964-06-11 1967-01-25 Cav Ltd Apparatus for supplying heated gases
GB1079733A (en) * 1963-01-07 1967-08-16 Continental Aviat & Eng Corp Fuel injection means for an internal combustion engine
GB1394856A (en) * 1972-07-13 1975-05-21 Teledyne Ind Fuel flow control unit for a gas turbine engine
GB1422981A (en) * 1972-01-03 1976-01-28 Eaton Corp Gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2492672A (en) * 1946-07-26 1949-12-27 Garrett Corp Turbine driven fluid circulating unit
FR1011066A (en) * 1948-11-30 1952-06-18 Combustion chamber
FR1119852A (en) * 1954-02-18 1956-06-26 Rolls Royce Improvements to gas turbine engine lubrication systems
DE1013467B (en) * 1955-07-30 1957-08-08 Daimler Benz Ag Combustion chamber for gas turbines and jet engines to sputter means
US2925215A (en) * 1957-06-20 1960-02-16 United Aircraft Corp Lubrication system
DE1162135B (en) * 1959-06-23 Power Jets Res & Dev Ltd Combustion chamber for gas turbine installations
US3018625A (en) * 1960-06-27 1962-01-30 Continental Aviat & Eng Corp Internal combustion turbine engine
GB1082232A (en) * 1964-09-05 1967-09-06 Continental Aviat & Eng Corp Gas turbine engine and rotary fuel injection means therefor
US3932988A (en) * 1972-10-25 1976-01-20 Beaufrere Albert H Fuel slinger combustor

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB699865A (en) * 1950-11-06 1953-11-18 W H Allen Sons & Company Ltd Improvements in or relating to gas turbines
GB727796A (en) * 1951-05-10 1955-04-06 Nat Res Dev Improvements relating to combustion equipment for burning liquid fuel and to gas turbine plant in which it is incorporated
GB719469A (en) * 1951-09-11 1954-12-01 Rolls Royce Improvements in or relating to fuel systems for internal combustion engines
GB837738A (en) * 1957-01-08 1960-06-15 Szydlowski Joseph Improvements in or relating to rotary injection devices for gas turbine combustion chambers
GB917704A (en) * 1958-07-31 1963-02-06 Power Jets Res & Dev Ltd Combustion apparatus
GB896223A (en) * 1959-05-22 1962-05-09 Bmw Triebwerkbau Gmbh Fuel induction through the rotor shaft of a gas turbine
GB955150A (en) * 1960-04-23 1964-04-15 Gasturbinenbau Und Energiemasc Improvements in or relating to gas turbines
GB1079733A (en) * 1963-01-07 1967-08-16 Continental Aviat & Eng Corp Fuel injection means for an internal combustion engine
GB1056338A (en) * 1964-06-11 1967-01-25 Cav Ltd Apparatus for supplying heated gases
GB1422981A (en) * 1972-01-03 1976-01-28 Eaton Corp Gas turbine engine
GB1394856A (en) * 1972-07-13 1975-05-21 Teledyne Ind Fuel flow control unit for a gas turbine engine

Also Published As

Publication number Publication date
DE3722530A1 (en) 1988-03-03
FR2602003A1 (en) 1988-01-29
GB8715321D0 (en) 1987-08-05
FR2602003B1 (en) 1993-12-17
IL83050A (en) 1993-01-31
US5042256A (en) 1991-08-27
DE3722530C2 (en) 1997-12-18
GB2197911A (en) 1988-06-02
IL83050D0 (en) 1987-12-31

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20040630